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NASA NTRS ยท 19930075302

Eigenvalue/Eigenvector derivatives for SAVI Gimbalflex nonlinear transient response analysis

Abstract

An eigenvector expansion method is utilized to predict eigenvalue and eigenvector derivatives due to geometric reconfiguration of a Gimbalflex fine-pointing/vibration isolation system called SAVI (Space Active Vibration Isolation). The eigenvector expansion method used is a modification of the classical method and allows for rigid body roots. Using the resulting modal derivatives, free-free nonlinear equations of motion are developed with Lagrange's Method. These equations represent a nonlinear plant model to be used in conjunction with a control system transient response simulation.

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BibTeXRIS

Orr, M. F., Jr.. 1988-03-24. Eigenvalue/Eigenvector derivatives for SAVI Gimbalflex nonlinear transient response analysis. https://ntrs.nasa.gov/citations/19930075302

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